Abstract
A theory is presented which predicts the post-failure behavior of laminated plates subjected to combined inplane loads. To take account of the post-failure state, two idealized material properties are assumed, i. e. , the ductile matrix and the brittle matrix. Throughout the process from the initial failure to the final fracture, the detailed behavior of the laminate can be analyzed. A method for analyzing the unloading and reloading behavior is also given.
| Original language | English |
|---|---|
| Title of host publication | Theoretical and Applied Mechanics |
| Publisher | Univ of Tokyo Press |
| Pages | 137-145 |
| Number of pages | 9 |
| ISBN (Print) | 4130660926 |
| Publication status | Published - Dec 1 1985 |
Publication series
| Name | Theoretical and Applied Mechanics |
|---|---|
| Volume | 33 |
| ISSN (Print) | 0285-6042 |
All Science Journal Classification (ASJC) codes
- Mechanics of Materials